Hybrid pressure deck for aircraft

Patent metadata

Field	Value
Publication number	US-11945568-B2
Application number	US-202217570288-A
Country	US
Kind code	B2
Filing date	Jan 6, 2022
Priority date	Mar 1, 2021
Publication date	Apr 2, 2024
Grant date	Apr 2, 2024

Abstract

Embodiments for hybrid pressure deck of an aircraft. One embodiment is a pressure deck disposed over a main gear wheel well of an aircraft. The pressure deck includes longitudinal beams extending in a forward and aft direction between an aft wheel well bulkhead and a rear spar of the aircraft. The pressure deck also includes a web attached to an underside of the longitudinal beams. The web includes a flat web portion supported by transverse stiffeners extending in an inboard and outboard direction, and a curved web portion including arches configured to flex laterally from load in the inboard and outboard direction. A transition between the flat web portion and the curved web portion extends at least partially in the forward and aft direction of the aircraft.

First claim

What is claimed is:

1. A pressure deck disposed over a main gear wheel well of an aircraft, the pressure deck comprising:
longitudinal beams extending in a forward and aft direction between an aft wheel well bulkhead and a rear spar of the aircraft a web attached to an underside of the longitudinal beams, the web including a flat web portion supported by transverse stiffeners extending in an inboard and outboard direction, and a curved web portion including arches configured to flex laterally from load in the inboard and outboard direction,
wherein a transition between a flat web portion and a curved web portion extends substantially diagonally with respect to the forward and aft direction such that a width of the flat web portion is full along the aft wheel well bulkhead and narrows toward a longitudinal center at the rear spar.

2. The pressure deck of claim 1 wherein:
the flat web portion is configured to provide a lateral load path proximate to the aft wheel well bulkhead, and
the curved web portion is configured to provide flexibility in the pressure deck at an area adjacent to the rear spar.

3. The pressure deck of claim 1 wherein:
the longitudinal beams are spaced from each other in an inboard and outboard direction between wheel well longeron beams at either side of body of the aircraft to form a middle bay, intermediate bays, and outboard bays,
the flat web portion is disposed in the middle bay and the outboard bays, and
a combination of the flat web portion and the curved web portion are disposed in the intermediate bays.

4. The pressure deck of claim 1 wherein:
the transverse stiffeners are disposed underneath the flat web portion.

5. The pressure deck of claim 1 wherein:
the flat web portion is co-cured with the transverse stiffeners.

6. A pressure deck disposed over a main gear wheel well of an aircraft, the pressure deck comprising:
longitudinal beams extending in a forward and aft direction between an aft wheel well bulkhead and a rear spar of the aircraft, the longitudinal beams spaced from each other in an inboard and outboard direction between wheel well longeron beams at either side of body of the aircraft to form a middle bay, intermediate bays, and outboard bays; and
a web attached to an underside of the longitudinal beams and the wheel well longeron beams, the web including a flat web portion supported by transverse stiffeners extending an inboard and outboard direction, and a curved web portion including arches configured to flex laterally under load in the inboard and outboard direction,
wherein a transition between the flat web portion and the curved web portion extends partially in the forward and aft direction of the aircraft,
wherein the flat web portion is disposed in the middle bay and the outboard bays to react side loads,
a width of the flat web portion is full along the aft wheel well bulkhead and narrows toward a longitudinal center at the rear spar, and
wherein a combination of the flat web portion and the curved web portion is disposed in the intermediate bays to provide flexibility at an intersection of the rear spar and the pressure deck.

7. The pressure deck of claim 6 wherein:
each of the arches extend between adjacent ones of the longitudinal beams to allow the pressure deck to flex laterally.

8. The pressure deck of claim 6 wherein:
the transverse stiffeners are disposed underneath the flat web portion.

9. The pressure deck of claim 6 wherein:
the flat web portion is co-cured with the transverse stiffeners.

10. The pressure deck of claim 1 wherein:
each of the arches extend between adjacent ones of the longitudinal beams to allow the pressure deck to flex laterally.

Assignees

• Boeing Co

Inventors

• Mclaughlin Mark R
• Leibov David H

Classifications

• B64C1/064

  Stringers; Longerons · CPC title

• B64C1/061

  Frames · CPC title

• B64C1/26

  Attaching the wing or tail units or stabilising surfaces · CPC title

• B64C1/18 Primary

  Floors · CPC title

• B64C1/10 Primary

  Bulkheads · CPC title